N305PC

Substantial
Serious

Raytheon Aircraft Company 1900DS/N: UE-299

Accident Details

Date
Friday, February 22, 2008
NTSB Number
SEA08LA082
Location
Kayenta, AZ
Event ID
20080228X00245
Coordinates
36.471668, -110.417778
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
2
Minor Injuries
3
Uninjured
15
Total Aboard
20

Probable Cause and Findings

The flight crew's failure to execute a missed approach, which resulted in a runway excursion after landing. Contributing to the accident were the inoperative lights, weather conditions below published approach minimums, and the slush contaminated runway.

Aircraft Information

Registration
N305PC
Make
RAYTHEON AIRCRAFT COMPANY
Serial Number
UE-299
Year Built
1997
Model / ICAO
1900D

Registered Owner (Historical)

Name
SALE REPORTED
Address
55 WESTPORT PLZ STE 640
Status
Deregistered
City
SAINT LOUIS
State / Zip Code
MO 63146-3132
Country
United States

Analysis

On February 22, 2008, about 0745 mountain standard time, a Raytheon Aircraft Company 1900D, N305PC, sustained substantial damage when it overran the runway during landing at Peabody Bedard Field Airport (38AZ), Kayenta, Arizona. The captain, first officer, and 13 of the 18 passengers were not injured. Two passengers received serious injuries and three passengers received minor injuries. The airplane was being operated by Peabody Energy, St. Louis, Missouri, under 14 Code of Federal Regulations Part 91. The purpose of the flight was to transport company personnel to the Black Mesa Coal Mine. Instrument meteorological conditions prevailed and an instrument flight rules (IFR) flight plan was filed. The flight departed from Flagstaff about 0700, and the intended destination was 38AZ.

According to information provided by the operator, the captain initially flew the GPS (global positioning system) runway 2 approach down to minimums and executed a missed approach. A second approach was made and the airplane touched down even with the midfield windsock. The captain applied brakes and full reverse on both propellers; however, the airplane did not slow down and continued off the end of the runway. The airplane impacted and knocked down a chain link fence and continued into downsloping rough terrain. The landing gear collapsed and the airplane slid to a stop. The operator reported that there was about 2 to 3 inches of slush on the runway.

The airport is privately owned and operated by Peabody Energy. The field elevation is 6,564 feet. There is one runway, runway 2/20, which has a paved asphalt surface that is 7,500 feet long by 75 feet wide. The runway is equipped with medium intensity runway lights, runway end identifier lights (REILs), and visual approach slope indicators that are pilot activated using the common traffic advisory frequency (122.8).

Review of the approach plate for the RNAV (GPS) runway 2 approach revealed that the minimums for the straight-in approach are 1 mile visibility, and a minimum descent altitude (MDA) of 6,860 feet mean sea level (329 feet agl). The missed approach point is the RWY02 waypoint, which is located at the threshold of runway 2. No alternative minimums to reflect inoperative lighting components are provided.

The airplane was equipped with a cockpit voice recorder (CVR) and a flight data recorder (FDR). The two recorders were removed from the airplane and sent to the National Transportation Safety Board laboratory in Washington, DC, for readout.

The FDR data indicates that the airplane lifted off around 0703, made a left turn to a northerly heading, and climbed to a cruise altitude of 17,000 feet. Around 0724, the airplane began to descend from cruise. The flaps were fully extended by 0728:22, and the recorded airspeed was 136 knots as the airplane was about to pass through 10,000 feet. Two minutes later, the autopilot parameter changed from engaged to disengaged. During the next minute, the pressure altitude remained around 6,800 feet for a period before it began to decrease again, recording a minimum value of 6,499 feet at 0731:25, and a recorded airspeed of 112 knots. The airplane pitch attitude and engine torque began to increase 2 seconds prior to the minimum recorded altitude value. The flaps were retracted as the airplane climbed, leveled off at 10,000 feet, and the autopilot reengaged around 0735.

The airplane began to descend again after 0740. The autopilot disengaged at 0744:05 as the pressure altitude reached 6,808 feet. Between 0744:30 and 0744:45, the engine torque was reduced, and the pressure altitude decreased from around 6,800 feet to about 6,500 feet. Based on the data recorded, the aircraft most likely touched down around 0744:48, with an airspeed of 112 knots. The left and right prop parameter indicated a reverse status within 2 seconds with the recorded airspeed at 106 knots. There was increased activity recorded on the vertical acceleration parameter over the next 15 seconds until the end of recorded data. The last recorded data point was at 0745, with an airspeed value of 31 knots. For further details of the data recorded by the FDR, see the public docket for this accident.

The audio information extracted from the CVR began at 0714:53 and continued to 0745:01. At 0718:47, the first officer commented, "hopefully the REILs are working, they weren't working yesterday." Between 0726:22 and 0731:23, conversation took place indicating the flight crew was performing the GPS Runway 2 approach and executing a missed approach. At 0735:47, the flight crew listened to the automated weather station at the airport, which was reporting, in part, "visibility one half [mile] light snow sky conditions ceiling two hundred broken one thousand overcast." At 0738:17, the first officer said, "I didn't see any lights on. I clicked them three separate times."

At 0737:40, the captain stated that he was starting the procedure turn, indicating the beginning of the second approach. At 0739:08, the captain stated that he was turning back inbound on the procedure turn. At 0740:15, the flight crew again listened to the automated weather station at the airport, which was reporting, in part, "visibility one half light snow sky conditions ceiling two hundred broken one thousand overcast." At 0744:09, the first officer said, "there's MDA," and at 0744:27, "there's the runway right below ya." The ground proximity warning system (GPWS) gave the audio alert, "sink rate, sink rate, sink rate, sink rate" at 0744:37. The area microphone recorded the sound of touchdown at 0744:52, and the sound of impact at 0745:00. A summary transcript of the entire recording is included in the public docket for this accident.

In a written statement, the captain described the termination of the second approach as follows: the first officer called the runway at 12 o'clock; they left the minimum descent altitude at 120 knots; and he landed about even with the midfield windsock. He braked and applied maximum reverse, but the aircraft did not slow down.

In a written statement, the first officer described the termination of the second approach as follows: we broke out and saw the end of the runway go below us. Could not see any lights, but saw the midfield windsock when the captain touched down. He started braking and there was zero effect. The captain went to full reverse and we were not slowing.

The airport is equipped with an Automated Weather Observation System (AWOS) that issued the following reports surrounding the period of the accident.

At 0715, wind from 170 degrees at 6 knots; visibility 2 miles in light snow, clouds scattered at 400 feet above ground level (agl), broken at 1,300 feet agl, overcast at 1,900 feet agl, temperature 0 degrees Celsius (C), dew point 0 degrees C, altimeter 29.99 inches of Mercury (Hg).

At 0720, wind from 170 degrees at 6 knots, visibility 1 and 1/4 miles in light snow; clouds scattered at 500 feet agl, broken at 1,300 feet agl, overcast at 1,900 feet agl; temperature 0 degrees Celsius (C); dew point 0 degrees C; altimeter 29.99 inHg.

At 0725, wind from 160 degrees at 7 knots; visibility 1 mile in unknown precipitation; clouds broken at 100 feet agl, broken at 500 feet agl, overcast at 1,400 agl; temperature 0 degrees Celsius (C); dew point 0 degrees C; altimeter 29.98 inHg.

At 0730, wind from 160 degrees at 8 knots; visibility 1 miles in light snow; clouds broken at 200 feet agl, overcast at 1,000 feet agl; temperature 0 degrees Celsius (C); dew point 0 degrees C; altimeter 29.98 inHg.

At 0735, wind from 170 degrees at 8 knots; visibility 3/4 mile in light snow; clouds broken at 200 agl, overcast at 1,000 feet agl; temperature 0 degrees Celsius (C); dew point 0 degrees C; altimeter 29.98 inHg.

At 0740, wind from 180 degrees at 9 knots; visibility 3/4 mile in unknown precipitation; clouds broken at 200 agl, overcast at 1,000 feet agl; temperature 0 degrees Celsius (C); dew point 0 degrees C; altimeter 29.98 inHg.

At 0745, wind from 180 degrees at 9 knots; visibility 1/2 mile in light snow; clouds broken at 100 feet agl, overcast at 1,000 feet agl; temperature 0 degrees Celsius (C); dew point 0 degrees C; altimeter 29.98 inHg.

At 0750, wind from 170 degrees at 8 knots; visibility 1/4 mile in light snow; clouds overcast at 100 feet; temperature 0 degrees Celsius (C); dew point 0 degrees C; altimeter 29.98 inHg.

At 0755, wind from 170 degrees at 8 knots; visibility 1/2 mile in light snow; clouds overcast at 100 feet; temperature 0 degrees Celsius (C); dew point 0 degrees C; altimeter 29.98 inHg.

Section 91.175 of the Federal Aviation Regulations specifies the flight rules applicable to takeoff and landing under IFR. Paragraphs (c), (d) and (e) state as follows:

(c) Operation below DA/DH or MDA. Except as provided in paragraph (l) of this section, where a DA/DH or MDA is applicable, no pilot may operate an aircraft, except a military aircraft of the United States, below the authorized MDA or continue an approach below the authorized DA/DH unless--

(1) The aircraft is continuously in a position from which a descent to a landing on the intended runway can be made at a normal rate of descent using normal maneuvers, and for operations conducted under part 121 or part 135 unless that descent rate will allow touchdown to occur within the touchdown zone of the runway of intended landing;

(2) The flight visibility is not less than the visibility prescribed in the standard instrument approach being used; and

(3) Except for a Category II or Category III approach where any necessary visual reference requirements are specified by the Administrator, at least one of the following visual references for the intended runway is distinctly visible and identifiable to the pilot:

(i) The approach light system, except that the pilot may not descend below 100 feet above the touchdown zone elevation using the approach lights as a reference unless the red terminating bars or...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA08LA082